The HyperTEK® is a modular, hybrid propellant rocket motor system that uses readily available nitrous oxide (N2O) and thermoplastic fuel grains. Designed primarily for use in launching small experimental payloads by universities, colleges, research institutes and sport rocketry enthusiasts, the system is also intended to be a technology demonstrator for CTI's and eAc's hybrid propulsion technology.

The HyperTEK® line of products has been sub-divided into the following sections:

For a downloadable copy
in PDF format of the complete HyperTEK® User's Manual, click here.

For a downloadable copy
in PDF format of all HyperTEK® system drawings
including dimensions, click here.

New Product
Specifications have been added to the J, L and M Series product
sections. Below are the Thrust Curves for the three different grain
sizes. Click on the graph to enlarge. Data files will be available here
very soon!